9783845405070 - Electro-hydrodynamic (EHD) Thrusters: Simulations, Analysis, and Optimization de Wan, Clemens (9 resultados)

Condición: New. pp. 120.

Taschenbuch. Condición: Neu. Electro-hydrodynamic (EHD) Thrusters | Simulations, Analysis, and Optimization | Clemens Wan | Taschenbuch | 120 S. | Englisch | 2011 | LAP LAMBERT Academic Publishing | EAN 9783845405070 | Verantwortliche Person für die EU: BoD - Books on Demand, In de Tarpen 42, 22848 Norderstedt, info[at]bod[dot]de | Anbieter: preigu.

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Taschenbuch. Condición: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -This paper presents the thrust optimization of Electro-hyrdodynamic (EHD) thrustersthrough theoretical, experimental, and simulation approaches. The underlying forceproduction theory is explained with electrical concepts, such as corona discharge, electrodepolarity, Corona Inception Voltage (CIV), and air breakdown principles. These concepts areapplied to the development of the theoretical derivation of the thrust equation relating thedesign variables in an EHD Thruster. The theoretical relationships derived were used toapproximate an EHD Thruster with the optimal force-to-weight ratio.Using the guiding design principles, a successful proof-of-concept EHD lifter modelwas built and tested. Although many of the design hypotheses were theoretically-sound, an updatedset of conclusions were expressed to explain and improve the failed trials with differentthruster geometries, electrode sizes, collector shapes, and various materials.The electrostatics, chargetransport, and hydrodynamics governing equations were implemented with the software toobtain graphical representations of the electric field and velocity airflow distributions of 2-Dand 3-D thruster models. 120 pp. Englisch.

Condición: New. Print on Demand pp. 120 2:B&W 6 x 9 in or 229 x 152 mm Perfect Bound on Creme w/Gloss Lam.

Condición: New. PRINT ON DEMAND pp. 120.

Condición: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Wan ClemensCooper Union Master s graduate with A.I. machine learning research experience in Osaka and Hamburg University. Currently working for an investment bank designing strategic solutions and exploring the components for a perfe.

Taschenbuch. Condición: Neu. This item is printed on demand - Print on Demand Titel. Neuware -This paper presents the thrust optimization of Electro-hyrdodynamic (EHD) thrustersthrough theoretical, experimental, and simulation approaches. The underlying forceproduction theory is explained with electrical concepts, such as corona discharge, electrodepolarity, Corona Inception Voltage (CIV), and air breakdown principles. These concepts areapplied to the development of the theoretical derivation of the thrust equation relating thedesign variables in an EHD Thruster. The theoretical relationships derived were used toapproximate an EHD Thruster with the optimal force-to-weight ratio.Using the guiding design principles, a successful proof-of-concept EHD lifter modelwas built and tested. Although many of the design hypotheses were theoretically-sound, an updatedset of conclusions were expressed to explain and improve the failed trials with differentthruster geometries, electrode sizes, collector shapes, and various materials.The electrostatics, chargetransport, and hydrodynamics governing equations were implemented with the software toobtain graphical representations of the electric field and velocity airflow distributions of 2-Dand 3-D thruster models.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 120 pp. Englisch.

Taschenbuch. Condición: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - This paper presents the thrust optimization of Electro-hyrdodynamic (EHD) thrustersthrough theoretical, experimental, and simulation approaches. The underlying forceproduction theory is explained with electrical concepts, such as corona discharge, electrodepolarity, Corona Inception Voltage (CIV), and air breakdown principles. These concepts areapplied to the development of the theoretical derivation of the thrust equation relating thedesign variables in an EHD Thruster. The theoretical relationships derived were used toapproximate an EHD Thruster with the optimal force-to-weight ratio.Using the guiding design principles, a successful proof-of-concept EHD lifter modelwas built and tested. Although many of the design hypotheses were theoretically-sound, an updatedset of conclusions were expressed to explain and improve the failed trials with differentthruster geometries, electrode sizes, collector shapes, and various materials.The electrostatics, chargetransport, and hydrodynamics governing equations were implemented with the software toobtain graphical representations of the electric field and velocity airflow distributions of 2-Dand 3-D thruster models.